View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 26266U 99057FC 22228.11775287 .00001926 00000-0 46065-3 0 9998
2 26266 98.5475 274.2067 0102175 100.8018 260.4697 14.51651213178621
| Epoch (UTC): | 16 August 2022 02:49:33 |
| Eccentricity: | 0.0102175 |
| inclination: | 98.5475° |
| perigee height: | 648 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 274.2067° |
| argument of perigee: | 100.8018° |
| revolutions per day: | 14.51651213 |
| mean anomaly at epoch: | 260.4697° |
| orbit number at epoch: | 17862 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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